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公开(公告)号:US08682509B2
公开(公告)日:2014-03-25
申请号:US12526431
申请日:2008-02-15
IPC分类号: G06F19/00
CPC分类号: G05B23/0283 , G07C5/008
摘要: A system to monitor aircraft equipment, having a chassis, defining an interior compartment, an arrangement configured to accept input data of at least one aircraft parameter, the arrangement configured to be placed within an aircraft, crash survivable cockpit voice and flight data recorder, and a power supply arrangement connected to arrangement configured to accept input data and the recorder.
摘要翻译: 一种用于监视飞机设备的系统,具有底盘,限定内部隔间,配置成接受至少一个飞机参数的输入数据的配置,被配置为放置在飞行器内的布置,碰撞存活的驾驶舱语音和飞行数据记录器,以及 连接到被配置为接受输入数据和记录器的配置的电源装置。
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公开(公告)号:US20100057277A1
公开(公告)日:2010-03-04
申请号:US12615974
申请日:2009-11-10
申请人: Jeff Goodrich , Paul Grabill , Tom Brotherton , Rob Luppold
发明人: Jeff Goodrich , Paul Grabill , Tom Brotherton , Rob Luppold
CPC分类号: B64F5/0045 , B64F5/60 , G07C5/085 , G07C5/0883
摘要: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
摘要翻译: 一种用于飞行器的健康监测的方法包括以下步骤:获得飞行器的振动数据,获得飞行器的导航数据,以及使用振动数据和导航数据确定飞机的健康状况。
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公开(公告)号:US08666569B2
公开(公告)日:2014-03-04
申请号:US12615974
申请日:2009-11-10
申请人: Jeff Goodrich , Paul Grabill , Tom Brotherton , Rob Luppold
发明人: Jeff Goodrich , Paul Grabill , Tom Brotherton , Rob Luppold
CPC分类号: B64F5/0045 , B64F5/60 , G07C5/085 , G07C5/0883
摘要: A method for health monitoring for an aircraft includes the steps of obtaining vibration data for the aircraft, obtaining navigation data for the aircraft, and determining a measure of health of the aircraft using the vibration data and the navigation data.
摘要翻译: 一种用于飞行器的健康监测的方法包括以下步骤:获得飞行器的振动数据,获得飞行器的导航数据,以及使用振动数据和导航数据确定飞机的健康状况。
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公开(公告)号:US08521341B2
公开(公告)日:2013-08-27
申请号:US12492944
申请日:2009-06-26
申请人: Tom Brotherton
发明人: Tom Brotherton
IPC分类号: G01C23/00
CPC分类号: G05D1/0055 , G05B23/0254
摘要: A method for fault determination for an aircraft includes the steps of generating a predicted maneuver of the aircraft using an aircraft operating input and a model of aircraft performance, determining an actual maneuver of the aircraft using information obtained from an inertial measurement system, comparing the predicted maneuver and the actual maneuver, and determining a fault of the aircraft based on the comparison of the predicted maneuver and the actual maneuver.
摘要翻译: 一种用于飞机的故障确定的方法包括以下步骤:使用飞行器操作输入和飞机性能模型来产生飞行器的预测机动,使用从惯性测量系统获得的信息确定飞行器的实际操纵,将预测的 基于预测机动和实际操纵的比较,确定飞机的故障。
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公开(公告)号:US20100332053A1
公开(公告)日:2010-12-30
申请号:US12492944
申请日:2009-06-26
申请人: Tom Brotherton
发明人: Tom Brotherton
IPC分类号: G06F7/00
CPC分类号: G05D1/0055 , G05B23/0254
摘要: A method for fault determination for an aircraft includes the steps of generating a predicted maneuver of the aircraft using an aircraft operating input and a model of aircraft performance, determining an actual maneuver of the aircraft using information obtained from an inertial measurement system, comparing the predicted maneuver and the actual maneuver, and determining a fault of the aircraft based on the comparison of the predicted maneuver and the actual maneuver.
摘要翻译: 一种用于飞机的故障确定的方法包括以下步骤:使用飞行器操作输入和飞机性能模型来产生飞行器的预测机动,使用从惯性测量系统获得的信息确定飞行器的实际操纵,将预测的 基于预测机动和实际操纵的比较,确定飞机的故障。
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公开(公告)号:US20110020122A1
公开(公告)日:2011-01-27
申请号:US12841301
申请日:2010-07-22
CPC分类号: F03D17/00 , F03D80/50 , F05B2230/80 , F05B2240/96 , F05B2270/804 , F05B2270/808 , F05B2270/81 , Y02E10/72 , Y02P70/523
摘要: A computer implemented method includes receiving condition information from a plurality of condition detection sensors coupled to a wind turbine and receiving wind turbine controller information. An anomaly detection algorithm is applied to identify maintenance activities for the wind turbine as a function of both the wind turbine condition information and the wind turbine controller information.
摘要翻译: 计算机实现的方法包括从耦合到风力涡轮机并接收风力涡轮机控制器信息的多个条件检测传感器接收条件信息。 应用异常检测算法来识别风力涡轮机的维护活动,作为风力涡轮机状况信息和风力涡轮机控制器信息的函数。
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